| Electric generator disposed on a rotating turboprop part G Bulin, S Perret, J Rogero US Patent 8,890,343, 2014 | 43 | 2014 |
| A genetic algorithms based optimisation tool for the preliminary design of gas turbine combustors JM Rogero Cranfield University, 2002 | 38 | 2002 |
| Application of genetic algorithm for preliminary trajectory optimization H Pervier, D Nalianda, R Espi, V Sethi, P Pilidis, D Zammit-Mangion, ... SAE International Journal of Aerospace 4 (2011-01-2594), 973-987, 2011 | 24 | 2011 |
| Assembly for aircraft comprising engines with boundary layer ingestion propulsion C Negulescu, J Rogero, R Faure US Patent 10,633,101, 2020 | 19 | 2020 |
| Optimization of combustor wall heat transfer and pollutant emissions for preliminary design using evolutionary techniques JM Rogero, PA Rubini Proceedings of the Institution of Mechanical Engineers, Part A: Journal of …, 2003 | 16 | 2003 |
| Structure establishing a sound insulator A Porte, J Rogero, AC MENDEZ US Patent App. 15/841,514, 2018 | 11 | 2018 |
| Deicing device for propfan-type propeller blades G Bulin, J Rogero, C Fabre US Patent 8,932,016, 2015 | 10 | 2015 |
| Engine assembly for an aircraft comprising a primary structure of a mounting pylon equipped with a box extension comprising two parts in the overall shape of an arch O Pautis, JM Rogero US Patent 10,017,267, 2018 | 9 | 2018 |
| Turbomachine comprising a heat management system J Rogero, O Verseux US Patent App. 15/667,873, 2018 | 8 | 2018 |
| Aircraft propulsion system having at least one anti-fire tank A Porte, JM Rogero US Patent 10,618,670, 2020 | 7 | 2020 |
| Applications of evolutionary algorithms for solving real-life design optimisation problems JM Rogero, A Tiwari, O Munaux, PA Rubini, R Roy, G Jared 6th Int. Conf. Parallel Problem Solving from Nature, Paris, France …, 2000 | 6 | 2000 |
| Spigot-type fastener provided with at least one means for measuring the force generated by an aircraft engine J Rogero, C Fabre, H Magnin US Patent 8,894,034, 2014 | 5 | 2014 |
| A mission assessment of aero engine losses O Thulin, T Grönstedt, JM Rogero ISABE-2015-20121, 2015 | 4 | 2015 |
| Aircraft propulsion assembly comprising a fan conjointly driven by two engines A Abele, J Rogero, J Guillemaut, M Belleville US Patent App. 15/919,970, 2018 | 3 | 2018 |
| Device for measuring a pattern of forces and moments generated by an aircraft propulsion system L Lafont, H Magnin, J Rogero US Patent 8,342,037, 2013 | 3 | 2013 |
| A platform independent engineering optimisation tool based on genetic algorithms and distributed computing applied to gas turbine combustor preliminary design JM Rogero, PA Rubini Computational engineering using metaphors from nature, 143-149, 2000 | 3 | 2000 |
| Aircraft propulsion assembly comprising two adjacent engines, of which the outlet nozzles have a straight portion in the vicinity of a median plane of the propulsion assembly C Negulescu, J Rogero US Patent 11,878,809, 2024 | 1 | 2024 |
| Aircraft engine assembly, comprising an attachment device for the engine equipped with a structural cover attached on a central box O Pautis, J Rogero US Patent 10,562,639, 2020 | 1 | 2020 |
| Drag decomposition of a subsonic wing via a far-field, exergy-based method DK Logothetis, PK Zachos, JM Rogero Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2023 | | 2023 |
